Computational Modeling of Mars Retropropulsion Concepts in the Langley Unitary Plan Wind Tunnel-Reference-Cited by-同舟云学术

Computational Modeling of Mars Retropropulsion Concepts in the Langley Unitary Plan Wind Tunnel

Published:2022-01-03 Issue: Volume: Page:
ISSN:
Container-title:AIAA SCITECH 2022 Forum
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Author:

Edquist Karl T.¹,Alter Stephen J.¹,Glass Christopher E.¹,Kleb William L.¹,Korzun Ashley M.¹,Wood William A.¹,Canabal Francisco²,Childs Robert³,Halstrom Logan D.³,Matsuno Kristen V.³

Affiliation:

1. NASA Langley Research Center

2. NASA Marshall Space Flight Center

3. NASA Ames Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0912

Reference41 articles.

1. Mars Exploration Entry, Descent, and Landing Challenges

2. Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems

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